A turbomachine combustor nozzle includes a first plate member having a first plurality of openings, and a second plate member having a second plurality of openings that are configured and disposed to be in alignment with the first plurality of openings. A plurality of nozzle members extends through corresponding ones of the first plurality of openings and the second plurality of openings. Each of the plurality of nozzle members includes a solid core.
FEDERAL RESEARCH STATEMENT
 This invention was made with Government support under Contract Number DE-FC26-05NT42643 awarded by the Department Of Energy. The Government has certain rights in this invention.